Title :
Simulation of proportional guidance law with an airship
Author :
Wei Gao ; Fen Lu
Author_Institution :
Beijing Inst. of Tracking & Telecommun. Technol., Beijing, China
Abstract :
A method for simulating missile guidance process with the unmanned airship piloted by a homing seeker is proposed and verified for the proportional guidance law by flight test. According to the airship control characteristics, we have designed the corresponding airship control law based on its ready PID controllers and successfully realized proportional guidance flight with the airship piloted by the line-of-sight angular rate signal produced by a TV seeker loaded on the airship. As an easy and economical technique for simulating missile guidance process, the method proposed here could have wide prospect of application in electronic warfare test and evaluation.
Keywords :
aircraft control; airships; electronic warfare; missile guidance; three-term control; PID controllers; TV seeker; airship control characteristics; airship control law design; electronic warfare test; flight test; homing seeker; line-of-sight angular rate signal; missile guidance process simulation; proportional guidance flight; proportional guidance law simulation; unmanned airship; Aerospace control; Atmospheric modeling; Jamming; Missiles; Safety; TV; Airship flight control; Electronic warfare test; Missile guidance simulation; Proportional law;
Conference_Titel :
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location :
Qingdao
Print_ISBN :
978-1-4799-7016-2
DOI :
10.1109/CCDC.2015.7162533
